Changed naming of the mixers to get rid of umbiguity as outputs are actually going to be driven by io, not fmu

Implemented automatic lookup for the .aux.mix file if it exists

1 files changed, 51 insertions, 0 deletions

diff --git a/ROMFS/px4fmu_common/mixers/wingwing.main.mix b/ROMFS/px4fmu_common/mixers/wingwing.main.mix
new file mode 100644
index 000000000..08333ba5c
--- /dev/null
+++ b/ROMFS/px4fmu_common/mixers/wingwing.main.mix
@@ -0,0 +1,51 @@
+Delta-wing mixer for PX4FMU
+===========================
+
+Designed for Wing Wing Z-84
+
+This file defines mixers suitable for controlling a delta wing aircraft using
+PX4FMU. The configuration assumes the elevon servos are connected to PX4FMU
+servo outputs 0 and 1 and the motor speed control to output 3. Output 2 is
+assumed to be unused.
+
+Inputs to the mixer come from channel group 0 (vehicle attitude), channels 0
+(roll), 1 (pitch) and 3 (thrust).
+
+See the README for more information on the scaler format.
+
+Elevon mixers
+-------------
+Three scalers total (output, roll, pitch).
+
+On the assumption that the two elevon servos are physically reversed, the pitch
+input is inverted between the two servos.
+
+The scaling factor for roll inputs is adjusted to implement differential travel
+for the elevons.
+
+M: 2
+O:      10000  10000      0 -10000  10000
+S: 0 0  -6000  -6000      0 -10000  10000
+S: 0 1   6500   6500      0 -10000  10000
+
+M: 2
+O:      10000  10000      0 -10000  10000
+S: 0 0  -6000  -6000      0 -10000  10000
+S: 0 1  -6500  -6500      0 -10000  10000
+
+Output 2
+--------
+This mixer is empty.
+
+Z:
+
+Motor speed mixer
+-----------------
+Two scalers total (output, thrust).
+
+This mixer generates a full-range output (-1 to 1) from an input in the (0 - 1)
+range.  Inputs below zero are treated as zero.
+
+M: 1
+O:      10000  10000      0 -10000  10000
+S: 0 3      0  20000 -10000 -10000  10000